Lean blowout precursor detection for gas turbines

US11713725B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11713725-B2
Application numberUS-202016885541-A
CountryUS
Kind codeB2
Filing dateMay 28, 2020
Priority dateMay 28, 2020
Publication dateAug 1, 2023
Grant dateAug 1, 2023

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A method for detecting blowout precursors in at least one gas turbine combustor comprising: receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis. Provided also is a system and a non-transitory computer readable medium configured to perform the method.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for detecting blowout precursors in at least one gas turbine combustor, comprising receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein said determining the existence of a blowout precursor comprises determining an increase in amplitude of time dependent spectral content in at least one predefined band of high frequency dynamics. 2. The method of claim 1 , wherein the band of high frequency dynamics is predefined based on an identification of bands of high frequency dynamics that appeared for the combustor approximately one second before a previous blowout event. 3. The method of claim 1 , wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient. 4. The method of claim 3 , further comprising using a windowed root-mean-square calculation to process the wavelet coefficient to determine the amplitude of the wavelet coefficient, and determining the existence of a blowout precursor based on an increased amplitude of the wavelet coefficient oscillation. 5. A system for acoustic detection of blowout precursors in at least one gas turbine combustor comprising an acoustic measuring device in communication with the combustor, wherein the acoustic measuring device generates signals indicative of acoustic combustion dynamics in the combustor in real time; and a blowout precursor monitoring unit that receives the acoustic signals and performs a simplified Mexican Hat wavelet transform analysis to detect the existence of a blowout precursor, wherein the blowout precursor monitoring unit detects the existence of a blowout precursor by determining an increase in amplitude of time dependent spectral content in at least one predefined band of high frequency dynamics. 6. The system as in claim 5 , further comprising a combustion controller configured to control at least one parameter of the operation of the combustor based at least in part on detection of a blowout precursor by the blowout precursor monitoring unit. 7. The system as in claim 6 , wherein the combustion controller is configured to generate at least one control signal upon detection of a blowout precursor to adjust a fuel-air ratio of fuel and air supplied to the combustor associated with the blowout precursor. 8. The system of claim 5 , wherein the at least one band of high frequency dynamics is predefined based on an identification of bands of high frequency dynamics that appeared for the combustor approximately one second before a previous blowout event. 9. The system of claim 5 , wherein the blowout precursor monitoring unit performs the wavelet analysis by determining the dominant frequencies of oscillation of the acoustic signal as a function of time to calculate a wavelet coefficient. 10. The system of claim 9 , wherein the blowout precursor monitoring unit uses a windowed root-mean-square calculation to process the wavelet coefficient to determine the amplitude of the wavelet coefficient, and detects the existence of a blowout precursor based on an increased amplitude of the wavelet coefficient oscillation. 11. The system of claim 5 , wherein the blowout precursor monitoring unit, upon detection of a blowout precursor, sends an alarm signal to an electronic device and/or sends a signal indicating the detection of the blowout precursor to a combustion controller. 12. A non-transitory computer-readable storage medium on which is encoded executable program code for performing a method for detecting blowout precursors in at least one gas turbine combustor comprising, receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein said determining the existence of a blowout precursor comprises determining an increase in amplitude of time dependent spectral content in at least one predefined band of high frequency dynamics. 13. The non-transitory computer readable medium of claim 12 , wherein the band of high frequency dynamics is predefined based on an identification of bands of high frequency dynamics that appeared for the combustor approximately one second before a previous blowout event. 14. The non-transitory computer readable medium of claim 12 , wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient. 15. The non-transitory computer readable medium of claim 14 , wherein the method further comprises using a windowed root-mean-square calculation to process the wavelet coefficient to determine the amplitude of the wavelet coefficient, and determining the existence of a blowout precursor based on an increased amplitude of the wavelet coefficient oscillation. 16. A method for detecting blowout precursors in at least one gas turbine combustor, comprising receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient. 17. A system for acoustic detection of blowout precursors in at least one gas turbine combustor comprising an acoustic measuring device in communication with the combustor, wherein the acoustic measuring device generates signals indicative of acoustic combustion dynamics in the combustor in real time; and a blowout precursor monitoring unit that receives the acoustic signals and performs a simplified Mexican Hat wavelet transform analysis to detect the existence of a blowout precursor, wherein the blowout precursor monitoring unit performs the wavelet analysis by determining the dominant frequencies of oscillation of the acoustic signal as a function of time to calculate a wavelet coefficient. 18. A non-transitory computer-readable storage medium on which is encoded executable program code for performing a method for detecting blowout precursors in at least one gas turbine combustor comprising, receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient.

Assignees

Inventors

Classifications

  • F02C9/50Primary

    with control of working fluid flow · CPC title

  • with provision for safeguarding the apparatus, e.g. against abnormal operation, against breakdown · CPC title

  • Measuring two or more variables by means not covered by a single other subclass · CPC title

  • of longitudinal or not specified vibrations · CPC title

  • by electric means (G01H3/14 takes precedence) · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US11713725B2 cover?
A method for detecting blowout precursors in at least one gas turbine combustor comprising: receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in…
Who is the assignee on this patent?
Electric Power Res Institute Inc
What technology area does this patent fall under?
Primary CPC classification F02C9/50. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 01 2023 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 7 related publications on this page (citations in our corpus or others sharing the same primary CPC).